Classifications

• • C—CHEMISTRY; METALLURGY
  • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
  • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
  • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
  • C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
  • C04B35/62204—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products using waste materials or refuse
  • C04B35/62213—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products using waste materials or refuse using rice material, e.g. bran or hulls or husks
• • C—CHEMISTRY; METALLURGY
  • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
  • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
  • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
  • C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
  • C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
  • C04B35/62605—Treating the starting powders individually or as mixtures
  • C04B35/62645—Thermal treatment of powders or mixtures thereof other than sintering
  • C04B35/6267—Pyrolysis, carbonisation or auto-combustion reactions
• • C—CHEMISTRY; METALLURGY
  • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
  • C10B—DESTRUCTIVE DISTILLATION OF CARBONACEOUS MATERIALS FOR PRODUCTION OF GAS, COKE, TAR, OR SIMILAR MATERIALS
  • C10B53/00—Destructive distillation, specially adapted for particular solid raw materials or solid raw materials in special form
• • C—CHEMISTRY; METALLURGY
  • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
  • C10B—DESTRUCTIVE DISTILLATION OF CARBONACEOUS MATERIALS FOR PRODUCTION OF GAS, COKE, TAR, OR SIMILAR MATERIALS
  • C10B57/00—Other carbonising or coking processes; Features of destructive distillation processes in general
  • C10B57/04—Other carbonising or coking processes; Features of destructive distillation processes in general using charges of special composition
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
  • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
  • F16C33/30—Parts of ball or roller bearings
  • F16C33/38—Ball cages
  • F16C33/44—Selection of substances
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
  • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
  • F16C33/30—Parts of ball or roller bearings
  • F16C33/66—Special parts or details in view of lubrication
  • F16C33/6603—Special parts or details in view of lubrication with grease as lubricant
  • F16C33/6607—Retaining the grease in or near the bearing
  • F16C33/6611—Retaining the grease in or near the bearing in a porous or resinous body, e.g. a cage impregnated with the grease
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
  • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
  • F16C33/30—Parts of ball or roller bearings
  • F16C33/66—Special parts or details in view of lubrication
  • F16C33/6637—Special parts or details in view of lubrication with liquid lubricant
  • F16C33/664—Retaining the liquid in or near the bearing
  • F16C33/6648—Retaining the liquid in or near the bearing in a porous or resinous body, e.g. a cage impregnated with the liquid
• • C—CHEMISTRY; METALLURGY
  • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
  • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
  • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
  • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
  • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
  • C04B2235/48—Organic compounds becoming part of a ceramic after heat treatment, e.g. carbonising phenol resins
• • C—CHEMISTRY; METALLURGY
  • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
  • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
  • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
  • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
  • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
  • C04B2235/54—Particle size related information
  • C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
  • C04B2235/5427—Particle size related information expressed by the size of the particles or aggregates thereof millimeter or submillimeter sized, i.e. larger than 0,1 mm
• • C—CHEMISTRY; METALLURGY
  • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
  • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
  • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
  • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
  • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
  • C04B2235/54—Particle size related information
  • C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
  • C04B2235/5436—Particle size related information expressed by the size of the particles or aggregates thereof micrometer sized, i.e. from 1 to 100 micron
• • C—CHEMISTRY; METALLURGY
  • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
  • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
  • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
  • C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
  • C04B2235/604—Pressing at temperatures other than sintering temperatures
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
  • Y02E50/00—Technologies for the production of fuel of non-fossil origin
  • Y02E50/10—Biofuels, e.g. bio-diesel

Definitions

• the present invention relates to a porous material suitable for use in a bearing retainer, obtained by a process comprising the steps of mixing degreased bran derived from rice bran with a thermosetting resin before kneading, subjecting a kneaded mixture to a primary firing in an inert gas at a temperature in a range of 700 to 1000°C, pulverizing the kneaded mixture obtained after the primary firing into carbonized powders sieved through a 60-mesh screen, mixing the carbonized powders with a thermosetting resin before kneading, pressure-forming a kneaded mixture thus obtained at a pressure in a range of 20 to 30 MPa, and applying a heat treatment again to a formed kneaded mixture in the inert gas at a temperature in a range of 100 to 1100°C.
• a carbonaceous material obtained by mixing and kneading degreased bran derived from rice bran with a thermosetting resin, drying a formed kneaded mixture prepared by pressure-forming, and firing the formed kneaded mixture as dried in an inert gas, and a method of forming the same.
• the inventors have been successful in development of a porous material suitable for use in fabricating a high-precision bearing retainer, having excellent properties as a material for use in fabricating a bearing retainer, and a small contraction ratio of the dimensions of a formed workpiece to those of a finished product.
• a porous material is obtained by a process comprising the steps of mixing degreased bran derived from rice bran with a thermosetting resin before kneading, subjecting a kneaded mixture to a primary firing in an inert gas at a temperature in a range of 700 to 1000°C, pulverizing the kneaded mixture obtained after the primary firing into carbonized powders sieved through a 60-mesh screen, mixing the carbonized powders with a thermosetting resin before kneading, pressure-forming a kneaded mixture thus obtained at a pressure in a range of 20 to 30 MPa, and applying a heat treatment again to a formed kneaded mixture in the inert gas at a temperature in a range of 100 to 1100°C, and the porous material thus obtained has not only ideal properties as a material suitable for use in a bearing retainer but also a small contraction ratio of the dimensions of a formed
• the porous material described above has the contraction ratio of the dimensions of the formed workpiece to those of the finished product as low as 3% or less, 13 wt % of oil retention characteristic, 4.85 x 10 -3 ⁇ cm of volume resistivity, and density in a range of 1.05 to 1.3 g / cm 3 , and further, it has been possible to obtain the porous material having suitable hardness, and still friction coefficient in the order of about 1. 05 after fired at a high temperature.
• Degreased bran derived from rice bran used in carrying out embodiments of the present invention, may be either of domestic origin or of foreign origin regardless of the kind of rice.
• thermosetting resin may be used as long as it has thermosetting property
• typically cited as a thermosetting resin are a phenol resin, diaryl phthalate resin, unsaturated polyester resin, epoxy resin, polyimide resin, and triazine resin.
• the phenol resin is preferably used.
• thermoplastic resin such as polyamide, and so forth can be used in combination with a thermosetting resin provided that it is done without departing from the spirit and scope of the invention.
• a proportion of the thermoplastic resin substituted for a portion of the thermosetting resin to the thermosetting resin is normally not more than 50 parts to 100 parts by weight.
• a mixing ratio of the degreased bran to the thermosetting resin is 50 ⁇ 90 : 50 ⁇ 10 by weight, however, a ratio of 75 : 25 is preferably used.
• thermosetting resin used in this case is preferably in a liquid state, having a relatively small molecular weight.
• a primary firing is applied at a temperature in a range of 700 to 100°C using normally a rotary kiln for a firing time in a range of 40 to 120 minutes.
• a mixing ratio of carbonized powders obtained after the primary firing to the thermosetting resin is 50 ⁇ 90 : 50 ⁇ 10 by weight, however, a ratio of 75 : 25 is preferably used.
• a kneaded mixture of the carbonized powders after the primary firing and the thermosetting resin is pressure-formed at a pressure in a range of 20 to 30 MPa, preferably in a range of 22 to 25 MPa.
• a mold is preferably at a temperature of about 150°C.
• thermoplastic resin can be substituted for a portion of the thermosetting resin, and in such a case, a mixing ratio is normally not more than 50 parts of the thermoplastic resin to 100 parts of the thermosetting resin by weight.
• a heat treatment is applied at a temperature in a range of 100 to 1100°C normally in a well-controlled electric furnace. Heat treatment time ranges from about 60 to 360 minutes.
• a warming rate up to a heat treatment temperature is required to be relatively moderate up to 500°C. In more specific terms, the warming rate is in a range of 0.5 to 2°C / min, preferably 1°C / min.
• a relatively moderate cooling rate is required up to 500°C.
• a cooling rate is in a range of 0.5 to 4°C / min, preferably 1°C / min.
• any of helium, argon, neon, and nitrogen gas may be used, however, nitrogen gas is preferably used.
• Embodiments of the invention are summed up as follows:
• the mixture was then fired at 900°C in a nitrogen atmosphere inside a rotary kiln for 60 minutes.
• a carbonized fired mixture thus obtained was pulverized by use of a crusher, and subsequently, was sieved through a screen of 60-mesh, thereby obtaining carbonized powders of particle size in a range of 50 ⁇ 250 ⁇ m.
• a formed mixture was taken out of the mold, heated in a nitrogen atmosphere at a warming rate of 1°C / min up to 500°C, held at 500°C for 60 min, and sintered at 900°C for about 120 min.
• the temperature of the formed mixture was lowered at a cooling rate in a range of 2 to 3°C / min up to 500°C, and upon the temperature dropping to 500°C or lower, the formed mixture was left to cool by itself.
• Table 1 shows various conditions of the process of producing the porous material for use in the bearing retainer. ex. 1 ex. 2 ex. 3 ex. 4 ex. 5 ex. 6 ex. 7 conv. ex. mix. amt. (g) degr'd bran 75 75 75 80 60 55 85 75 t-sett. resin 25 25 25 20 40 35 15 25 prim. firing (°C ) 900 900 900 850 1000 1000 800 - time (min) 60 60 60 60 70 70 60 aver. particle size ( ⁇ m) 90 90 90 40 120 50 130 - mix. amt. (g) 75 75 75 75 75 75 80 85 - c.powder t-sett. resin 25 25 25 25 25 20 15 form. press.
• Table 2 shows properties of the porous material suitable for use in the bearing retainer, produced according to the examples of production, 1 to 7, and a conventional example. ex. 1 ex. 2 ex. 3 ex. 4 ex. 5 ex. 6 ex. 7 conv. ex. d. c. ratio (%) 2.0 2.5 2.4 1.9 1.8 1.75 1.25 25 c. s. (MPa) 103 150 140 95 110 115 95 60 oil ret. wt % 13.3 9.8 10.0 14.1 12.8 12.8 14.5 13.5 vol. res'st. (10 -3 ⁇ cm) 4.85 49.0 47.5 6.2 5.9 3.1 4.9 1.4 fr'ctn coeff.
• Compressive strength was measured by conducting tests on testpieces in a columnar shape of 5 mm (diameter) x 12.5 mm (height). Oil retention characteristic is indicated by a ratio of weight of lubricating oil to that of the testpiece as measured by means of centrifugal separation of the lubricating oil from the testpiece impregnated with the lubricating oil as deaerated at 1150 rpm for 45 seconds. Hygroscopicity was measured by heating the testpiece at 150°C for 6 hours, and treating the same in a vacuum desiccator for 20 hours before leaving the same in a room at room temperature for 72 hours.
• Table 3 shows friction coefficient. load 50 Hz 10 N * 0.19 - 0.26 50 N * 0.33 - 0.4 10 N # 0.16 - 0.22 50 N # 0.27 - 0.34 Remarks: * without lubricating oil; # with lubricating oil
• Friction coefficient was found by use of a SRV tester at 1 mm stroke at room temperature, using a steel ball 10 mm in diameter, and applying a load either 10N or 50N.
• a formed mixture was taken out of the mold, heated in a nitrogen atmosphere at a warming rate of 1°C / min up to 500°C, and sintered at 900°C for about 120 min.
• the temperature of the formed mixture was lowered at a cooling rate in a range of 2 to 3°C / min up to 500°C, and upon the temperature dropping to 500°C or lower, the formed mixture was left to cool by itself.
• Table 2 shows properties thereof.
• the porous material suitable for use in the bearing retainer according to the invention has novel properties not observed of the conventional material, such as a small contraction ratio of the dimensions of a formed workpiece to those of a finished product, excellent hot oil resistance, small thermal strain, insusceptibility to damage, light weight, a long service life, and still ability to retain oil and grease for a long period of time.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• General Engineering & Computer Science (AREA)
• Organic Chemistry (AREA)
• Manufacturing & Machinery (AREA)
• Ceramic Engineering (AREA)
• Materials Engineering (AREA)
• Mechanical Engineering (AREA)
• Oil, Petroleum & Natural Gas (AREA)
• Structural Engineering (AREA)
• Inorganic Chemistry (AREA)
• Chemical Kinetics & Catalysis (AREA)
• Combustion & Propulsion (AREA)
• Physics & Mathematics (AREA)
• Thermal Sciences (AREA)
• Rolling Contact Bearings (AREA)
• Carbon And Carbon Compounds (AREA)
• Coke Industry (AREA)
• Ceramic Products (AREA)
• Porous Artificial Stone Or Porous Ceramic Products (AREA)

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• 2000
  • 2000-12-15 JP JP2000382236A patent/JP2002187773A/ja not_active Withdrawn
• 2001
  • 2001-11-21 US US09/990,431 patent/US6395677B1/en not_active Expired - Fee Related
  • 2001-12-07 EP EP01129133A patent/EP1215409A3/fr not_active Withdrawn

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